A Practical Guide to 'Free-Energy' Devices

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Fig.11 is an exploded, perspective view which illustrates the main components of the filter portion of the vapour equaliser of the present invention. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT Referring now to the drawings, where parts are numbered the same in each drawing, and more particularly to Fig.1 which illustrates a preferred embodiment of the present invention as installed in a motor vehicle. The preferred embodiment includes as its main components a fuel vapour tank 10 in which the fuel vapour is stored and generated for subsequent delivery to the internal combustion engine 20. On the top of fuel vapour tank 10 is mounted an air inlet control valve 12 whose structure and operation will be described in greater detail below. The internal combustion engine 20 includes a standard intake manifold 18. Mounted upon the intake manifold 18 is a vapour equaliser chamber 16. Connected between the fuel vapour tank 10 and the vapour equaliser chamber 16 is a vapour conduit or hose 14 for conducting the vapours from within tank 10 to the chamber 16. Reference numeral 22 indicates generally an air inlet control valve which is mounted on the vapour equaliser chamber 16. Thus, the system is provided with two separate air inlet control valves 12 and 22 which are respectively coupled via cables 24 and 26 to the throttle control for the motor vehicle which may take the form of a standard accelerator pedal 28. The air inlet control valves 12 and 22 are synchronised in such a fashion that the opening of the air inlet control valve 22 of the vapour equaliser 16 always precedes and exceeds the opening of the air inlet control valve 12 of the fuel vapour tank 10, for reasons which will become more clear later. A - 962
The cooling system of the vehicle conventionally includes a radiator 30 for storing liquid coolant which is circulated through the engine 20 in the well-known fashion. A pair of hoses 32 and 34 are preferably coupled into the normal heater lines from the engine 20 so as to direct heated liquid coolant from the engine 20 to a warming coil 36, preferably constructed of copper, which is positioned within vapour tank 10. I have found that the water circulation system consisting of hoses 32, 34 and 36 serves three distinct functions. Firstly, it prevents the vapour tank from reaching the cold temperatures to which it would otherwise be subjected as a result of high vacuum pressure and air flow through it. Secondly, the heated coolant serves to enhance vaporisation of the fuel stored within tank 10 by raising its temperature. Thirdly, the liquid coolant, after leaving tank 10 via conduit 34, has been cooled to the point where engine 20 may then be run at substantially lower operating temperatures to further increase efficiency and prolong the life of the engine. Included in series with vapour conduit 14 is a filter unit 38 which is designed to retard the flow of fuel vapour from the tank 10 to the vapour equaliser 16. The precise structure of the filter unit 38 will be described in greater detail below. A thrust adjustment valve 40 is positioned upstream of the filter unit 38 in conduit 14 and acts as a fine adjustment for the idling speed of the vehicle. Positioned on the other side of filter unit 38 in conduit 14 is a safety shut-off valve 42 which comprises a one-way valve. Starting the engine 20 will open the valve 42 to permit the engine vacuum pressure to be transmitted to tank 10, but, for example, a backfire will close the valve to prevent a possible explosion. The tank 10 may also be provided with a drain 44 positioned at the bottom of the tank. Positioned on the side of the vapour equaliser chamber 16 is a primer connection 46 which may be controlled by a dash mounted primer control knob 48 connected to tank 10 via conduit 47. A conduit 50 extends from the oil breather cap opening 52 in a valve cover 54 of the engine 20 to the vapour equaliser 16 to feed the oil blow-by to the engine as a means for eliminating valve clatter. This is believed necessary due to the extreme lean mixture of fuel vapour and air fed to the combustion cylinders of the engine 20 in accordance with the present invention. Referring now to Fig.2 and Fig.3, the fuel vapour tank 10 of the present invention is illustrated in greater detail in orthogonal sectional views and is seen to include a pair of side walls 56 and 58 which are preferably comprised of heavy duty steel plate (e.g. 1/2" thick) in order to withstand the high vacuum pressures developed inside it. Tank 10 further comprises top wall 60 and bottom wall 62, and front and rear walls 64 and 66, respectively. In the front wall 64 of tank 10 is positioned a coupling 68 for mating the heater hose 32 with the internal copper conduit 36. Tank 10 is also provided with a pair of vertically oriented planar support plates 70 and 72 which are positioned somewhat inside the side walls 56 and 58 and are substantially parallel to them. Support plates 70 and 72 lend structural integrity to the tank 10 and are also provided with a plurality of openings 74 (Fig.2) at the bottom of them to permit fluid communication through it. The bottom of tank 10 is generally filled with from one to five gallons of fuel, and the walls of tank 10 along with plates 70 and 72 define three tank chambers 76, 78 and 80 which are, by virtue of openings 74, in fluid communication with one another. In the top wall 60 of tank 10 is formed an opening 82 for placing one end of vapour conduit 14 in fluid communication with the interior chamber 76 of tank 10. A second opening 84 is positioned in the top wall 60 of tank 10 over which the air inlet control valve 12 is positioned. The valve assembly 12 comprises a pair of conventional butterfly valves 86 and 88 which are coupled via a control rod 90 to a control arm 92. Control arm 92 is, in turn, pivoted under the control of a cable 24 and is movable between a solid line position indicated in Fig.2 by reference numeral 92 and a dotted line position indicated in Fig.2 by reference numeral 92’. Rod 90 and valves 86 and 88 are journaled in a housing 94 having a base plate 96 which is mounted on a cover 98. As seen in Fig.1, the base plate 96 includes several small air intake ports or apertures 100 formed on both sides of the butterfly valves 86 and 88, which are utilised for a purpose to become more clear later on. Rod 90 is also journaled in a flange 102 which is mounted to cover 98, while a return spring 104 for control arm 92 is journaled to cover 98 via flange 106. Extending through the baffle and support plates 70 and 72 from the side chambers 78 and 80 of tank 10 to be in fluid communication with apertures 100 are a pair of air conduits 108 and 110 each having a reed valve 112 and 114 positioned at the ends, for controlling air and vapour flow through it. The reed valves 112 and 114 cooperage with the small apertures 100 formed in the base plate 96 to provide the proper amount of air into the tank 10 while the engine is idling and the butterfly valves 86 and 88 are closed. Mounted to the front wall 64 of tank 10 is a pivot support member 132 for pivotally receiving a filter element which is indicated generally by reference numeral 134 and is illustrated in a perspective, partially cut away view in Fig.5. The unique, pivotable filter element 134 comprises a frame member 136 having a pin-receiving stub 138 extending along one side member of it. The actual filter material contained within the frame 136 comprises a layer of carbon particles 148 which is sandwiched between a pair of layers of sponge-like filter material which A - 963
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JUAN AGUERO Patent Application EP04
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the exhaust manifold. This heats so
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combustion chambers. The hydrogen i
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21. The system of claim 20, charact
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electrolysis of water at such a rat
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Fig.4 is an elevation view of the h
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Fig.10 is a cross-section on the li
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Fig.16 is a cross-section on the li
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Fig.23 is an enlargement of part of
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Fig.33 is a perspective view of a v
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A - 843
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through a resistor R4 to provide tr
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The installation of the above circu
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cathode in the upper region of the
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transformer and, assuming an input
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valve apparatus to control engine s
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. a first hollow cylindrical electr
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CHRISTOPHER ECCLES UK Patent App. 2
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Fig.1 is a circuit diagram of fract
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If a large electric field is applie
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The pulses R1 and S1 are of the sam
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DISCLOSURE OF THE INVENTION The inv
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A - 867
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Fig.5B shows a stylised representat
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Fig.6 shows a gas collection system
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Fig.8A and Fig.8B are views of a se
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A - 875
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Figs.16-30 are graphs supporting th
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A - 879
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A - 881
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A - 883
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A - 885
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A - 887
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If it is the case that the hydrogen
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plate shown in Fig.1A and Fig.1B an
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is in equilibrium where the 10 watt
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The previously mentioned prior art
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The stores of high pressure gases c
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unit to retain operational gas pres
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HENRY PAINE This is a very interest
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Henry Paine’s apparatus would the
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some form of distortion of space. I
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superconductive disk is made part o
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Fig.2A and Fig.2B are diagrams, pre
Page 89 and 90: Fig.4A and Fig.4B are diagrams, pre
Page 91 and 92: #1 hollow superconductive shield #2
Page 93 and 94: Fig.2B shows the counter-clockwise
Page 95 and 96: In this example, the difference bet
Page 97 and 98: CHARLES POGUE US Patent 642,434 12t
Page 99 and 100: Fig.3 is a horizontal sectional vie
Page 101 and 102: Fig.9 and Fig.10 are detail section
Page 103 and 104: having a valve 52 in it. Chamber 50
Page 105 and 106: CHARLES POGUE US Patent 1,997,497 9
Page 107 and 108: Fig.4 is a detail sectional view of
Page 109 and 110: A low-speed or idling jet 25 has it
Page 111 and 112: DESCRIPTION OF THE DRAWINGS Fig.1 i
Page 113 and 114: Fig.5 is a detail sectional view on
Page 115 and 116: Vapour formed by air bubbling throu
Page 117 and 118: From the foregoing description it w
Page 119 and 120: Fig.2 is an enlarged view of the de
Page 121 and 122: Fig.6 is a section taken along line
Page 123 and 124: ROBERT SHELTON US Patent 2,982,528
Page 125 and 126: Fig.4 is a transverse sectional vie
Page 127 and 128: HAROLD SCHWARTZ US Patent 3,294,381
Page 129 and 130: 182,420 now abandoned. The present
Page 131 and 132: DESCRIPTION OF THE INVENTION The ca
Page 133 and 134: THOMAS OGLE US Patent 4,177,779 11t
Page 135 and 136: In accordance with other aspects of
Page 137 and 138: Fig.3 is a sectional view of the va
Page 139: Fig.7 is a partial side, partial se
Page 143 and 144: Upon initial starting of the engine
Page 145 and 146: (f) A filter positioned in the vapo
Page 147 and 148: with the magnitude of the current a
Page 149 and 150: Fig.1B is a perspective view of the
Page 151 and 152: Fig.3 is a top view of the motor of
Page 153 and 154: Fig.7 is an isometric view showing
Page 155 and 156: Fig.10 is a top view showing the ro
Page 157 and 158: Fig.13 is a top view of a pair of r
Page 159 and 160: Extending in opposite diametric dir
Page 161 and 162: Fig.5 shows the state of the switch
Page 163 and 164: otor magnets 42 - 49 when in the ho
Page 165 and 166: Fig.9 and Fig.10 show a second arra
Page 167 and 168: constructed otherwise than as speci
Page 169 and 170: 12. The motor of claim 11 wherein t
Page 171 and 172: timer or a control mechanism mounte
Page 173 and 174: Fig.4 is a view similar to Fig.3 bu
Page 175 and 176: Fig.10 is a view similar to Fig.3 f
Page 177 and 178: Fig.13 is a schematic circuit diagr
Page 179 and 180: Fig.16 is a simplified embodiment o
Page 181 and 182: Fig.22 to Fig.25 are similar to Fig
Page 183 and 184: Referring to Fig.2, the permanent m
Page 185 and 186: Fig.7 shows a modified embodiment w
Page 187 and 188: them, will depend upon the order in
Page 189 and 190: Fig.14, shows another embodiment 14
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Fig.18 shows the air coil 210 posit
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Figs. 22-25 show four different pos
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movement with the first permanent m
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a shaft and means journaling the sh
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CLAUDE MEAD and WILLIAM HOLMES US P
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Fig.2 is a front elevation of the w
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impactors and drills. The turbine d
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(a) fourth rotating means responsiv
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path to the other side of the perma
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Fig.3 is an oscilloscope waveform t
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DETAILED DESCRIPTION OF THE PREFERR
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although it is by no means obvious
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second diode connected at its posit
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In the present invention, a permane
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Fig.4 is a circuit diagram, illustr
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and Fig.3. In practice, this coil m
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y a simultaneous magnetic accelerat
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Mr. P.G. Mallory started out in 191
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All models have a 30 Watt power rat
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In the auto racing circles it has a
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BATTERY + _ SIMPLIFIED MULTIVIBRATO
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Schematic Wiring Diagrams for two P
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motor. What is not generally known,
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Mark McKay's investigation of Edwin
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Investor Photo #012D Popping a coil
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capacitors connected in series, wit
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PULSE WIDTH TIME IN mS went to the
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TOP DEAD CENTER 0° REFERENCE Accor
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The recovery and simple analysis of
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FILTER CAPACITOR + 2 OHM 200 WATT R
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Subject: CSET design Date: Sun Feb
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Date: Fri Feb 28, 2003 8:25 pm (Tim
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(Tad Johnson) I'm being as careful
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SANGAMO ENERGY DISCHARGE CAPACITOR
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(Alan Francoeur) But I also measure
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Subject: Progress Date: Sun Mar 30,
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● all electrical connections were
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Mark Gray claims that the heart and
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Mark Gray claims that some potentia
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Radio Frequency (RF) Generator Gene
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Some time during 1987 - 1988, Gray
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The two-channel trace from the osci
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What “maximum squareness” means
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Zo = 112 Ohms Td of 293 nS. 50 KV 8
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MIKE BRADY’S “PERENDEV” MAGNE
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Fig.3 is a perspective view showing
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Fig.7 is a perspective view showing
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In the rotor assembly 30 of Fig.2,
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Fig.7 shows a typical magnetic sour
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DONALD A. KELLY ABSTRACT Patent US
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This series of magnetic oscillating
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Because there is no natural, lock-i
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Fig.3 is an enlarged top view of on
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An arm 9, is fastened to a flat fac
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Fig.2 is a vertical transverse cros
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Fig.6 is a vertical, longitudinal,
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Working inside the cylinders 12 are
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Leroy K. Rogers Patent US 4,292,804
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Preferred embodiments of a method a
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Fig.6 is a cross-sectional view of
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tapped hole in the cylinder 20 typi
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A second embodiment of a valve actu
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otates faster, the other end 98 of
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In normal operation (as seen in Fig
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Eber Van Valkinburg Patent US 3,744
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Referring to the drawings in detail
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Since the pump depends for its supp
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Briefly, in one aspect the engine o
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Fig.12 is a cross-sectional view si
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Fig.14 is a schematic diagram of an
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A - 1163
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A - 1165
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Figs.20A-20F are schematic diagrams
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Note: Corresponding reference chara
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Integral with the piston bodies are
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The piston has a generally semi-tor
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Referring back to Fig.13A, for engi
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As piston 39A reaches BDC, distribu
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mixture and do not combine because
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These wires are about twelve gauge,
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cold-cathode tube 391, and an x-ray
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Fig.17D), polariser 289, branch B17
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Robert Britt US Patent 3,977,191 31
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Fig.3 is an elevational view of the
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Fig.7 is an electrical schematic of
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Referring now to Fig.3 of the drawi
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and drives Q1 into conduction. The
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Floyd Sweet Recently, some addition
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The day when we witnessed the VTA d
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up to see Floyd. Floyd was with the
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Energy cannot enter a space of zero
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electromagnetic and gravitational f
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or in another form: So, the e.m.f.
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Example 2: Suppose the conductor wi
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Meguer Kalfaian There is a patent a
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Fig.2 illustrates a controlled top
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Fig.9 is a modification of Fig.6; a
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the outer periphery of the magnet,
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wobbling top is sufficient, as proo
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Theodore Annis & Patrick Eberly US
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BRIEF DESCRIPTION OF THE DRAWINGS F
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Fig.6 is a schematic diagram of a s
Page 405 and 406:
DETAILED DESCRIPTION OF THE PREFERR
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Fig.5 is a detail drawing of an alt
Page 409 and 410:
In the preferred implementation of
Page 411 and 412:
William McDavid junior US Patent 6,
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This sloping floor causes the drive
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FIG.3 is a side elevational view of
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FIG.9 is a horizontal cross-section
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otational downstream annular chambe
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In Fig.5 is shown a perspective vie
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small hydro-electric version of the
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Fig.10 is a perspective view of a s
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longitudinally mounted in the upstr
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shaft in the central aperture, said
Page 431 and 432:
Scientific Papers The following lin
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